Daher Tbm 910 vs Daher Tbm 960 vs Pilatus Pc 12 Ngx vs Piper M600 Sls
In category, the Daher TBM 910 and TBM 960 are very fast, pressurized single‑engine turboprops optimized for owner‑pilots and efficient point‑to‑point travel, with the TBM 960 being the newer, more refined flagship. The Pilatus PC‑12 NGX is also a pressurized single‑engine turboprop, but it sits in a larger “utility/business” class, prioritizing cabin volume, payload flexibility, and rugged operations. The Piper M600 SLS is a pressurized single‑engine turboprop positioned below the TBM and PC‑12 in size and speed, emphasizing simpler operation and lower acquisition/operating costs. For range, the TBM 960 and TBM 910 generally lead this group, typically offering around the 1,500–1,700 nautical mile class depending on reserves and cruise settings. The PC‑12 NGX is competitive, often around the 1,500‑nautical‑mile class, but its real advantage is carrying more while still going far. The M600 SLS is usually shorter‑legged, roughly around the 1,000–1,400 nautical mile class depending on configuration. For passenger capacity, the TBMs and M600 commonly seat about 4–6 passengers in comfort (with additional seats possible in some layouts), while the PC‑12 NGX typically accommodates more, often 6–9, with the most cabin and baggage flexibility.
| Spec | Daher TBM 910 | Daher TBM 960 | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.25 | $ 2.78 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Daher TBM | Pilatus | Piper |
| Aircraft Name | TBM 910 | TBM 960 | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1730 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.56 | $ 0.56 | $ 0.46 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 2908 | 2908 | — | 2200 |
| Standard Cabin Seats | 4 | 4 | 6 | 4 |
| Direct Operating Cost | $ 744 | $ 744 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 330 | 290 | 274 |
| Base Aircraft Price (USD) | $4,250,000 | $4,450,000 | $5,350,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — | — |
| Max Cabin Seats | — | — | 9 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | No | Optional | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 5 |
| Galley Location | MID | MID | — | MID |
| Cabin Pressure (psi) | 6.2 | 6.2 | 5.8 | 5.6 |
| Galley / Refreshment | Refreshment Centre | — | No | Refreshment Centre |
| Standard Cabin Seats | 4 | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 14390 | 14390 | 13100 | 12600 |
| Cargo Door | — | — | Yes | — |
| Max Cabin Seats | — | — | 9 | — |
| Lavatory Location | — | — | FWD | — |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PT6A-66D | TBM 960 | PT6E-67XP | PT6A-42A |
| TBO (hrs) | 3500 | 3500 | 5000 | 3600 |
| Horsepower | 850 | 850 | 1200 | 600 |
| Flat Rating | ISA + 49 | ISA + 49 | ISA + 35 | ISA + 55 |
| No. of Engines | 1 | — | 1 | 1 |
| Fuel Burn (gph) | 37 | — | — | — |
| Fuel Capacity (gal) | 291 | — | — | 260 |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 35.3 | 35.3 | 47.25 | 29.7 |
| Wingspan (ft) | 42.1 | 42.1 | 53.33 | 43.2 |
| Cabin Width (ft) | 4 | 4 | 5 | 4.1 |
| Cabin Height (ft) | 4.1 | 4.1 | 4.9 | 4 |
| Cabin Length (ft) | 13.4 | 13.4 | 16.9 | 12.3 |
| Overall Height (ft) | 14.3 | — | 14 | 11.3 |
| Cabin Volume (cu. ft) | 123 | 123 | — | 165 |
| Baggage Volume Int. (cu. ft) | 30 | — | 40 | 20 |
| Cabin Width - Floor (ft) | — | — | 4.25 | — |